| タイトル | NASA Langley developments in response calculations needed for failure and life prediction |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940018148 |
| 著者（英） | Housner, Jerrold M. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-10-01 |
| 言語 | eng |
| 内容記述 | NASA Langley developments in response calculations needed for failure and life predictions are discussed. Topics covered include: structural failure analysis in concurrent engineering; accuracy of independent regional modeling demonstrated on classical example; functional interface method accurately joins incompatible finite element models; interface method for insertion of local detail modeling extended to curve pressurized fuselage window panel; interface concept for joining structural regions; motivation for coupled 2D-3D analysis; compression panel with discontinuous stiffener coupled 2D-3D model and axial surface strains at the middle of the hat stiffener; use of adaptive refinement with multiple methods; adaptive mesh refinement; and studies on quantity effect of bow-type initial imperfections on reliability of stiffened panels. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 94N22621 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/114564 |
